Aerodynamics Equipment for Training Manufacturer, Suppliers and Exporter in India
Educational Instrument is leading Aerodynamics Equipment for Training Manufacturer,and supplier and Exporter in India, Algeria (Algiers), Angola (Luanda), Argentina (Buenos Aires), Armenia (Yerevan), Australia(Canberra), Austria (Vienna), Bahrain (Manama), Bangladesh (Dhaka), Bhutan (Thimphu), Bolivia (Sucre), Botswana (Gaborone), Brazil (Brasília), Brunei (Bandar Seri Begawan), Montenegro (Podgorica), Morocco (Rabat), Mozambique (Maputo), Myanmar (Naypyidaw), Namibia (Windhoek), Nepal (Kathmandu), New Zealand (Wellington), Nigeria (Abuja), Oman (Muscat), Palestine (Ramallah), Panama (Panama City), Papua New Guinea (Port Moresby), Paraguay (Asunción), Peru (Lima), Philippines (Manila)¸ Portugal (Lisbon), Qatar (Doha), Rwanda (Kigali), Saudi Arabia (Riyadh), Senegal (Dakar), Serbia (Belgrade), Sierra Leone (Freetown), Slovakia (Bratislava), South Africa (Cape Town) (Pretoria) (Bloemfontein), South Sudan (Juba), Spain (Madrid), Sri Lanka (Sri Jayawardenepura Kotte) (Colombo), Sudan (Khartoum), Syria (Damascus), Tanzania (Dodoma), Thailand (Bangkok), Togo (Lomé), Tonga (Nuku'alofa), Trinidad and Tobago (Port of Spain), Tunisia (Tunis), Turkey (Ankara), Turkmenistan (Ashgabat), Uganda (Kampala), United Arab Emirates (Abu Dhabi), United Kingdom (London), United States (Washington, D.C.)
Aerodynamics equipment for training comprises laboratory systems, wind tunnels, aerodynamic models, measuring instruments and airflow experiment modules used to study air movement, lift, drag, pressure, boundary layers, turbulent jets and flow visualization. Educational manufacturer & Exporter, presents this category for school, university, TVET, research and industry requirements.
The collection includes subsonic and bench-top wind tunnels, a modular air flow bench, aircraft and aerofoil models, drag and boundary-layer modules, pressure-measurement equipment, balances, a smoke generator and related experimental accessories. The supplied category page lists 27 product entries with codes spanning EL-AEFT-11243 to EL-AEFT-11270. Buyers should select equipment according to the aerodynamic principle being investigated, wind-tunnel compatibility, pressure-measurement requirements, experimental model type and any optional instrumentation required. Specifications not stated in the supplied category information should be requested before procurement.
What aerodynamics equipment is available for training laboratories?
The category includes wind tunnels, airflow benches, aircraft and aerofoil models, drag models, boundary-layer modules, pressure-measurement equipment, flow-visualization accessories and aerodynamic balances. The supplied category page lists 27 product entries, including two separately coded Subsonic Wind Tunnels and several experiment modules for airflow investigation. ilable aerodynamics-focused products include:
- Subsonic Wind Tunnel — EL-AEFT-11250
- Wind Tunnel — EL-AEFT-11245
- Modular Air Flow Bench — EL-AEFT-11249
- Bench Top Wind Tunnel — EL-AEFT-11251
- Subsonic Wind Tunnel — EL-AEFT-11252
- Flutter Wing — EL-AEFT-11253
- Aircraft Model — EL-AEFT-11254
- Three Dimensional Drag Models — EL-AEFT-11255
- Aerofoil with Tappings — EL-AEFT-11256
- Flat Plate Boundary Layer Model Roughened and Smooth — EL-AEFT-11257
- Bernoulli Equation — EL-AEFT-11258
- Drag Force — EL-AEFT-11259
- Round Turbulent Jet — EL-AEFT-11260
- Aero foil with Pressure Tapings — EL-AEFT-11261
- Flat Plate Drag Model — EL-AEFT-11262
- Boundary Layer — EL-AEFT-11263
- Flow Visualization — EL-AEFT-11264
- Multi Tube Manometer — EL-AEFT-11265
- Smoke Generator — EL-AEFT-11266
- Three Component Balance — EL-AEFT-11267
- Differential Pressure Unit — EL-AEFT-11268
- 32-Way Pressure Unit — EL-AEFT-11269
- Basic And Drag Balance — EL-AEFT-11270
The category page also lists four communications and data products that require verification for category relevance before publication. How do you choose aerodynamics equipment for a training laboratory?
Choose aerodynamics equipment by matching the apparatus to the intended experiment: wind-tunnel investigation, lift and drag measurement, aerofoil pressure study, boundary-layer analysis, turbulent-jet work, Bernoulli equation demonstration or airflow visualization. Buyers should also verify whether the selected model requires a wind tunnel, pressure instrument, balance or other ancillary equipment. general airflow studies, the category includes several wind tunnels and a Modular Air Flow Bench. Aircraft and aerofoil experiments can use the Aircraft Model, Aerofoil with Tappings and Aero foil with Pressure Tapings. Drag-related options include Three Dimensional Drag Models, Drag Force and Flat Plate Drag Model.
Pressure investigations can involve the Multi Tube Manometer, Differential Pressure Unit or optional 32-Way Pressure Unit. The Smoke Generator supports visual observation of airflow in subsonic wind tunnels and other low-flow-rate airflow products.
Where compatibility or complete specifications are not stated, request product-specific technical information before ordering.
Which wind tunnels are available in this aerodynamics collection?
The category lists four wind-tunnel entries: a compact open-circuit suction Subsonic Wind Tunnel, a general Wind Tunnel, a Bench Top Wind Tunnel and another Subsonic Wind Tunnel with separate control and instrumentation. Each product has a distinct product code and description. first Subsonic Wind Tunnel, code EL-AEFT-11250, is described as a compact, practical open-circuit suction wind tunnel for studying aerodynamics.
The Bench Top Wind Tunnel, code EL-AEFT-11251, uses a bench-mounting metal frame that holds all parts of the wind tunnel in one compact unit.
The second Subsonic Wind Tunnel, code EL-AEFT-11252, uses a separate control and instrumentation unit to control axial-fan speed and air velocity in the working section.
The general Wind Tunnel, code EL-AEFT-11245, is listed without further functional detail on the category page.
Which products are used to study lift, drag and aerodynamic forces?
The Aircraft Model, Three Dimensional Drag Models, Drag Force module, Flat Plate Drag Model and aerodynamic balances support different investigations involving lift, drag, pitching moment or aerodynamic forces. Selection depends on the model being tested and the measurement arrangement required. Aircraft Model is described for experiments involving lift, drag and pitching moment of fixed-wing aircraft. The Flat Plate Drag Model demonstrates flow around a bluff body mounted normal to the airflow direction.
The Three Component Balance attaches to the vertical wall of the wind-tunnel working section. The Basic And Drag Balance allows test models with a rigid support arm to be mounted and held securely within the wind-tunnel working section.
Complete force ranges, model dimensions, measurement accuracy and wind-tunnel compatibility are not stated in the supplied category information and should be requested before procurement.
Which equipment is available for aerofoil and pressure-distribution experiments?
The collection includes an Aerofoil with Tappings, an Aero foil with Pressure Tapings, a Multi Tube Manometer, Differential Pressure Unit and 32-Way Pressure Unit for pressure-related aerodynamic investigations. Buyers should verify compatibility between the test model, pressure tubing and measuring instrument before ordering. Aerofoil with Tappings, code EL-AEFT-11256, has 20 static pressure tappings along its chord on the upper and lower surfaces.
The separately listed Aero foil with Pressure Tapings, code EL-AEFT-11261, allows students to connect tubes to other optional pressure-measurement instruments.
The Multi Tube Manometer uses clean water as its working fluid. The 32-Way Pressure Unit is described as an optional ancillary for modular Subsonic Wind Tunnels.
Detailed compatibility information should be requested where the supplied category page does not identify the exact wind-tunnel or model combinations.
Which equipment supports boundary-layer, jet and airflow studies?
The Flat Plate Boundary Layer Model Roughened and Smooth, Boundary Layer module, Round Turbulent Jet, Bernoulli Equation module and Flow Visualization module cover different airflow and fluid-dynamics investigations represented in this category. Each addresses a specific flow phenomenon or experimental arrangement. Bernoulli Equation module illustrates the Bernoulli equation as applied to a convergent-divergent duct. The Round Turbulent Jet module consists of a tube with a specially designed rounded entry.
The Boundary Layer module consists of a duct containing a flat plate. The Flow Visualization module uses a specially shaped duct with a large working section and transparent window.
A separate Flat Plate Boundary Layer Model Roughened and Smooth is also listed. Detailed construction, measuring points, dimensions and instrumentation requirements are not provided in the category summary and should be requested where required.
How can airflow be visualized in a subsonic wind tunnel?
The Smoke Generator is intended to let students see airflow in subsonic wind tunnels and other low-flow-rate airflow products. The category also includes a Flow Visualization module with a specially shaped duct, a large working section and a transparent window. Smoke Generator is listed under product code EL-AEFT-11266. The Flow Visualization module is listed under EL-AEFT-11264.
These two products represent different approaches within the supplied catalogue: one generates smoke for observing airflow, while the other provides a duct and transparent viewing area for flow-visualization work.
Operating requirements, smoke medium, compatibility and included accessories are not stated in the category summary. Specifications should therefore be requested before equipment selection or tender submission.
What should buyers verify before ordering aerodynamics training equipment?
Buyers should verify the experimental objective, wind-tunnel type, test model, pressure-measurement method, required balance, optional accessories, system compatibility and complete technical specification before placing an order. Several products in this category are described as models, modules or ancillaries that may form part of a larger experimental arrangement. example, the 32-Way Pressure Unit is an optional ancillary to modular Subsonic Wind Tunnels. The Aero foil with Pressure Tapings can connect to optional pressure-measurement instruments. The Three Component Balance attaches to a wind-tunnel working section, while the Basic And Drag Balance holds suitable test models within the working section.
Institutions preparing specifications or tenders should therefore confirm product compatibility, included equipment, dimensions, measurement ranges, electrical requirements and any ancillary components where these details are not stated.
Does Educational Instruments export aerodynamics equipment internationally?
Yes. Educational Instruments is supplied in the input as a Manufacturer & Exporter, and the company states that its distributor and dealer network extends across more than 82 countries. Its About Us page identifies engineering laboratory equipment among the equipment categories it manufactures and exports. supplied aerodynamics category page lists markets across Africa, Asia, Europe, the Middle East, Oceania, North America and South America. The FAQ also states that international export is available for educational laboratory equipment. institutional or export enquiries, buyers should provide the required product names, product codes, quantities and technical requirements when requesting a formal quotation.
Aerodynamics Equipment Types
|
Type |
Key feature stated in supplied information |
Typical use |
|
Subsonic Wind Tunnel — EL-AEFT-11250 |
Compact open-circuit suction wind tunnel |
Aerodynamics study |
|
Wind Tunnel — EL-AEFT-11245 |
Listed as a wind tunnel |
Wind-tunnel experiments |
|
Modular Air Flow Bench — EL-AEFT-11249 |
Steel framework with a mounted fan |
Airflow experiments |
|
Bench Top Wind Tunnel — EL-AEFT-11251 |
Bench-mounting metal frame holds the system in one compact unit |
Bench-scale wind-tunnel work |
|
Subsonic Wind Tunnel — EL-AEFT-11252 |
Separate control and instrumentation unit controls axial-fan speed and air velocity |
Controlled subsonic airflow study |
|
Flutter Wing — EL-AEFT-11253 |
Represents wing flutter as a combination of forces |
Wing-flutter investigation |
|
Aircraft Model — EL-AEFT-11254 |
Intended for lift, drag and pitching-moment experiments |
Fixed-wing aircraft experiments |
|
Three Dimensional Drag Models — EL-AEFT-11255 |
Three-dimensional aerodynamic drag models |
Drag experiments |
|
Aerofoil with Tappings — EL-AEFT-11256 |
20 static pressure tappings along the chord on upper and lower surfaces |
Aerofoil pressure investigation |
|
Flat Plate Boundary Layer Model Roughened and Smooth — EL-AEFT-11257 |
Roughened and smooth flat-plate boundary-layer model |
Boundary-layer comparison |
|
Bernoulli Equation — EL-AEFT-11258 |
Convergent-divergent duct experiment module |
Bernoulli equation demonstration |
|
Drag Force — EL-AEFT-11259 |
Duct with transparent front and rear |
Drag-force experiment |
|
Round Turbulent Jet — EL-AEFT-11260 |
Tube with specially designed rounded entry |
Turbulent-jet study |
|
Aero foil with Pressure Tapings — EL-AEFT-11261 |
Tubes can connect to optional pressure-measurement instruments |
Aerofoil pressure experiments |
|
Flat Plate Drag Model — EL-AEFT-11262 |
Shows flow around a bluff body normal to airflow |
Bluff-body drag study |
|
Boundary Layer — EL-AEFT-11263 |
Duct containing a flat plate |
Boundary-layer experiments |
|
Flow Visualization — EL-AEFT-11264 |
Specially shaped duct with large working section and transparent window |
Airflow visualization |
|
Multi Tube Manometer — EL-AEFT-11265 |
Uses clean water as working fluid |
Multi-point pressure measurement |
|
Smoke Generator — EL-AEFT-11266 |
Allows students to see airflow in subsonic wind tunnels and low-flow-rate products |
Airflow visualization |
|
Three Component Balance — EL-AEFT-11267 |
Attaches to the vertical wall of a wind-tunnel working section |
Aerodynamic-force measurement |
|
Differential Pressure Unit — EL-AEFT-11268 |
Listed as a differential-pressure unit |
Differential-pressure measurement |
|
32-Way Pressure Unit — EL-AEFT-11269 |
Optional ancillary to modular Subsonic Wind Tunnels |
Multi-channel pressure display |
|
Basic And Drag Balance — EL-AEFT-11270 |
Holds test models with rigid support arms in the wind-tunnel working section |
Drag and model-testing experiments |
Product names, codes and stated features in this table are taken from the supplied category page. Aerodynamics Equipment Selection Criteria
|
Criterion |
What to check |
|
Experimental objective |
Identify whether the requirement concerns wind tunnels, lift, drag, pitching moment, boundary layers, turbulent jets, Bernoulli equation, pressure or flow visualization. |
|
Wind-tunnel configuration |
Compare the listed general, bench-top, open-circuit suction and instrumented subsonic wind-tunnel options. |
|
Test model |
Determine whether an aircraft, aerofoil, flat plate, drag model, flutter wing or other model is required. |
|
Pressure measurement |
Check whether the experiment requires pressure tappings, a multi-tube manometer, differential-pressure unit or 32-way pressure unit. |
|
Balance requirement |
Determine whether a Three Component Balance or Basic And Drag Balance is needed for the intended test arrangement. |
|
Flow visualization |
Compare the Smoke Generator and Flow Visualization module according to the experimental method. |
|
Ancillary compatibility |
Confirm whether the selected item is standalone or is an optional ancillary for another system. |
|
Product identification |
Use the exact product name and code shown on the category page. |
|
Missing specifications |
Request dimensions, ranges, accuracies, electrical requirements, included accessories and compatibility details where not stated. |
These selection criteria are based only on the products and functional descriptions supplied on the category page. Related Educational Instruments Pages
Frequently Asked Questions
1. What is aerodynamics equipment for training?
Aerodynamics training equipment consists of laboratory instruments and experimental systems used to study airflow and aerodynamic principles. Typical equipment includes wind tunnels, aerofoil models, aircraft models, pressure measurement devices, aerodynamic balances, smoke generators, and flow visualization accessories for experiments involving lift, drag, pressure distribution, boundary layers, turbulent jets, and airflow behavior.
2. How many products are available in the Aerodynamics Equipment for Training category?
The category contains 27 product listings with product codes ranging from EL-AEFT-11243 to EL-AEFT-11270. Since some product codes are not sequential, buyers should refer to the product list when requesting quotations.
3. Which equipment is suitable for lift, drag, and pitching-moment experiments?
The Aircraft Model is specifically designed for experiments measuring lift, drag, and pitching moment of fixed-wing aircraft. Other related equipment includes:
- Three Dimensional Drag Models
- Drag Force Module
- Flat Plate Drag Model
- Aerodynamic Balances
4. How many pressure tappings does the Aerofoil with Tappings have?
The Aerofoil with Tappings (Product Code: EL-AEFT-11256) features 20 static pressure tappings positioned along the upper and lower surfaces of the aerofoil chord for pressure distribution experiments.
5. Which equipment is used for airflow visualization?
Airflow can be visualized using:
- Smoke Generator – Produces visible smoke for observing airflow in subsonic wind tunnels and low-speed airflow experiments.
- Flow Visualization Module – Features a transparent working section for studying airflow patterns within a specially designed duct.
6. What working fluid does the Multi Tube Manometer use?
The Multi Tube Manometer (Product Code: EL-AEFT-11265) uses clean water as its working fluid, providing a safe and convenient method for pressure measurement during laboratory experiments.
7. Is the 32-Way Pressure Unit a standalone wind tunnel?
No. The 32-Way Pressure Unit is an optional accessory designed for use with compatible modular Subsonic Wind Tunnel systems. It is not a standalone wind tunnel and should be matched with the appropriate equipment.+
Request a Quote with the required product names, product codes, quantities and technical requirements.
Subsonic Wind Tunnel
Product Code : EL-AEFT-11250
A compact, practical open-circuit suction wind tunnel for studying aerodynamics.
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Data Acquisition Systems
Product Code : EL-AEFT-11243
Data Acquisition Systems OPC server will read the raw data which was received by communication server application.
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Modular Air Flow Bench
Product Code : EL-AEFT-11249
The unit consists of a sturdy steel framework on which is mounted a fan.
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Analogue Communications Trainer
Product Code : EL-AEFT-11247
Analogue Communications Trainer.
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Amplitude Modulation And Demodulation Kit
Product Code : EL-AEFT-11248
Amplitude Modulation And Demodulation Kit
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Bench Top Wind Tunnel
Product Code : EL-AEFT-11251
A bench-mounting metal frame holds all parts of the wind tunnel in one compact unit.
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Subsonic Wind Tunnel
Product Code : EL-AEFT-11252
A separate control and instrumentation unit controls the speed of the axial fan (and the air velocity in the working section).
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Flutter Wing
Product Code : EL-AEFT-11253
Wing flutter is a complex event that arises from a combination of forces.
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Aircraft Model
Product Code : EL-AEFT-11254
This model is good for experiments with lift, drag and pitching moment of fixed wing aircraft.
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Three Dimensional Drag Models
Product Code : EL-AEFT-11255
Three Dimensional Drag Models.
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Aerofoil with Tappings
Product Code : EL-AEFT-11256
The aero foil has 20 static pressure tappings along its chord on the upper and lower surfaces.
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Flat Plate Boundary Layer Model Roughened and Smooth
Product Code : EL-AEFT-11257
Flat Plate Boundary Layer Model Roughened and Smooth.
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Bernoulli Equation
Product Code : EL-AEFT-11258
This experiment module illustrates Bernoulli equation as applied to a convergent-divergent duct.
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Drag Force
Product Code : EL-AEFT-11259
This simple yet comprehensive experiment module consists of a duct with transparent front and rear.
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Round Turbulent Jet
Product Code : EL-AEFT-11260
This module consists of a tube with a specially designed rounded entry.
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Aero foil with Pressure Tapings
Product Code : EL-AEFT-11261
Students can connect the tubes to other optional pressure-measurement instruments.
View Details
Flat Plate Drag Model
Product Code : EL-AEFT-11262
This model shows the flow around a bluff body mounted normal to the air flow direction.
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Boundary Layer
Product Code : EL-AEFT-11263
This module consists of a duct in which there is situated a flat plate.
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Flow Visualization
Product Code : EL-AEFT-11264
This module consists of a specially-shaped duct which has a large working section with transparent window.
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Multi Tube Manometer
Product Code : EL-AEFT-11265
The manometer uses clean water as a working fluid for safety and convenience.
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Smoke Generator
Product Code : EL-AEFT-11266
A smoke generator and probe that allows students to see air flow in subsonic wind tunnels and other low flow rate air flow products.
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Three Component Balance
Product Code : EL-AEFT-11267
The balance attaches to the vertical wall of the wind tunnel working section.
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32-Way Pressure Unit
Product Code : EL-AEFT-11269
The 32-Way Pressure Display Unit is an optional ancillary to modular Subsonic Wind Tunnels.
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Basic And Drag Balance
Product Code : EL-AEFT-11270
The balance mechanism enables test models with a rigid support arm to be mounted and held securely in position in the working section of the wind tunnel.
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